ZlatanKapidˇzi´c Strengthanalysisandmodelingofhybridcomposite-aluminumaircraftstructures

• After numerical search, results obtained through IFF failure analysis for LC Tension when the influence of (σ 11 ) stresses is

Micromechanical Model to Investigate the Influence of Fiber Properties,” Report 493, Department of Solid Mechanics, Royal Institute of Technology,

Jolma: “Residual strength of impact damaged scaled down CFRP-foam core sandwich panels” Bull conducted the analysis and the testing of the sandwich panels loaded in in-plane

(a) Solidification of Aluminum at 4s and 6s respectively from the start of the filling of the mold with calculating Discrete Random Walk Model, 6mm inlet diameter; (b)

The need for uncertainty management and more complete validation methods that complement traditional validation, knowledge of a model’s maturity and simulation result accuracy, has

increases. The decreased forced also means that the Bohr radius increases. Exciton binding energies are on the order of 0.1-1 eV and 0.01-0.1 eV for Frenkel and Wannier-

Based on this knowledge, the aircraft industry has developed methods for securing the fatigue durability, the damage growth tolerance and the static and residual strength of

Copyright c  2015 by Zlatan Kapidˇzi´c ISBN 978-91-7685-942-1